Title:
折りたたみ支柱を有する着陸装置を作動させる方法
Document Type and Number:
Japanese Patent JP5457551
Kind Code:
B2
Abstract:
A method of operating an aircraft landing gear between a deployed position and a retracted position. The landing gear comprises a leg hinged to the aircraft, the leg being stabilized in the deployed position by a folding strut comprising two hinged-together links, the strut being held in an aligned position by a stabilizer member comprising two hinged-together links themselves held in alignment by a locking member. The method comprises the steps of arranging the strut (2; 102) and the stabilizer member (4; 104) in such a manner that at least one of the links (4a; 104a) of the stabilizer member moves continuously during a movement of the leg from the deployed position to the retracted position, and of attaching an operating actuator (10; 110) to the link in order to cause the link to pivot against the locking member and to exert thereon a force tending to move the leg.
Inventors:
Nikola Keller
Albert de Pandray
Edouard Campbell
Dominic duco
Sebastian dubois
Albert de Pandray
Edouard Campbell
Dominic duco
Sebastian dubois
Application Number:
JP2012513625A
Publication Date:
April 02, 2014
Filing Date:
June 03, 2010
Export Citation:
Assignee:
Messier-Bugatti-Douti
International Classes:
B64C25/14
Domestic Patent References:
| JP2011513138A | ||||
| JP62168792A | ||||
| JP2006509675A | ||||
| JP10129596A |
Foreign References:
| US5022609 | ||||
| US2222975 | ||||
| FR2801865A1 |
Attorney, Agent or Firm:
Atsushi Aoki
Tetsuro Shimada
Shinji Mitsuhashi
Takuya Shinoda
Yoryo Mihashi
Yuichi Morimoto
Tetsuro Shimada
Shinji Mitsuhashi
Takuya Shinoda
Yoryo Mihashi
Yuichi Morimoto